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Perturbation Theory

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Perturbation Theory Orbital Dynamics and Attitude Control EuMAS-European Masters Course in Aeronautics and Space Technology Dr. Rafael Ramis Abril – PowerPoint PPT presentation

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Title: Perturbation Theory


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  • The transformation from cartesian variables to
    Delaunay variables is canonical
  • M, ?, and ? are coordinates and ?, h, and hz
    their momentums
  • See section 4, R. Ramis, Mecánica Orbital y
    Dinámica de Actitud, ETSIA
  • See chapter 8, F. T. Geyling and H. R. Westerman,
    Introduction to Orbital Mechanics, Chapter 8,
    Addison-Wesley

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Example constant radial force
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System of ODE to be solved numerically
Numerical (truncation) error g DtN, instead
DtN
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First order equations can be reduced to
integrals
Equation for M1 must be integrated after equation
for a1
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Sometimes integrals can be evaluated analytically
The parameter variations include secular and
oscilatory terms
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rmax
e
rmin
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